id
int64 0
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stringlengths 36
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stringlengths 17
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int64 0
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| choices
listlengths 3
6
| labels
listlengths 3
6
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stringlengths 72
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| expected_output
stringlengths 4
285
|
|---|---|---|---|---|---|---|---|
173
|
a7800b29-9996-40ff-9b1f-f6a35588d522
|
Which of the following was the first known SAR in space?
| 2
|
[
"TRMM",
"ICESAT",
"SEASAT",
"CALIPSO"
] |
[
0,
0,
1,
0
] |
Which of the following was the first known SAR in space?
A. TRMM
B. ICESAT
C. SEASAT
D. CALIPSO
|
C. SEASAT
|
174
|
1e3d4af8-4eaf-4730-8155-fb1a9cab4ecf
|
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
| 0
|
[
"Lateral Chromatic",
"Astigmatism",
"Length Chromatic",
"Curvature of Field",
"Spherical"
] |
[
1,
0,
1,
0,
1
] |
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
A. Lateral Chromatic
B. Astigmatism
C. Length Chromatic
D. Curvature of Field
E. Spherical
|
A. Lateral Chromatic
C. Length Chromatic
E. Spherical
|
174
|
1e3d4af8-4eaf-4730-8155-fb1a9cab4ecf
|
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
| 1
|
[
"Length Chromatic",
"Spherical",
"Astigmatism",
"Lateral Chromatic",
"Curvature of Field"
] |
[
1,
1,
0,
1,
0
] |
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
A. Length Chromatic
B. Spherical
C. Astigmatism
D. Lateral Chromatic
E. Curvature of Field
|
A. Length Chromatic
B. Spherical
D. Lateral Chromatic
|
174
|
1e3d4af8-4eaf-4730-8155-fb1a9cab4ecf
|
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
| 2
|
[
"Astigmatism",
"Length Chromatic",
"Lateral Chromatic",
"Spherical",
"Curvature of Field"
] |
[
0,
1,
1,
1,
0
] |
Which of the following aberrations can be fully corrected by Doublet/Schmidt optical systems?
A. Astigmatism
B. Length Chromatic
C. Lateral Chromatic
D. Spherical
E. Curvature of Field
|
B. Length Chromatic
C. Lateral Chromatic
D. Spherical
|
175
|
c68460d2-8cd8-4f88-a407-6cc47d3af00d
|
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
| 0
|
[
"Lens Doublet",
"TMA (Three-mirror anastigmatic)",
"Schmidt",
"Cassegrain"
] |
[
0,
0,
0,
1
] |
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
A. Lens Doublet
B. TMA (Three-mirror anastigmatic)
C. Schmidt
D. Cassegrain
|
D. Cassegrain
|
175
|
c68460d2-8cd8-4f88-a407-6cc47d3af00d
|
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
| 1
|
[
"Cassegrain",
"TMA (Three-mirror anastigmatic)",
"Lens Doublet",
"Schmidt"
] |
[
1,
0,
0,
0
] |
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
A. Cassegrain
B. TMA (Three-mirror anastigmatic)
C. Lens Doublet
D. Schmidt
|
A. Cassegrain
|
175
|
c68460d2-8cd8-4f88-a407-6cc47d3af00d
|
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
| 2
|
[
"Schmidt",
"Lens Doublet",
"TMA (Three-mirror anastigmatic)",
"Cassegrain"
] |
[
0,
0,
0,
1
] |
Which of the following reflective optical system is analogous to the Tele-optic refractive optical system?
A. Schmidt
B. Lens Doublet
C. TMA (Three-mirror anastigmatic)
D. Cassegrain
|
D. Cassegrain
|
176
|
881245b2-6dfa-4b39-93fa-454b10919ef7
|
Which of the following best describe a spherical aberration?
| 0
|
[
"when a sharp image is formed on a focal surface which isn't flat",
"when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center",
"dispersion of the light due to the refractive index of a lens being a function of the wavelength",
"when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane"
] |
[
0,
1,
0,
0
] |
Which of the following best describe a spherical aberration?
A. when a sharp image is formed on a focal surface which isn't flat
B. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
C. dispersion of the light due to the refractive index of a lens being a function of the wavelength
D. when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane
|
B. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
|
176
|
881245b2-6dfa-4b39-93fa-454b10919ef7
|
Which of the following best describe a spherical aberration?
| 1
|
[
"when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane",
"when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center",
"when a sharp image is formed on a focal surface which isn't flat",
"dispersion of the light due to the refractive index of a lens being a function of the wavelength"
] |
[
0,
1,
0,
0
] |
Which of the following best describe a spherical aberration?
A. when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane
B. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
C. when a sharp image is formed on a focal surface which isn't flat
D. dispersion of the light due to the refractive index of a lens being a function of the wavelength
|
B. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
|
176
|
881245b2-6dfa-4b39-93fa-454b10919ef7
|
Which of the following best describe a spherical aberration?
| 2
|
[
"when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center",
"dispersion of the light due to the refractive index of a lens being a function of the wavelength",
"when a sharp image is formed on a focal surface which isn't flat",
"when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane"
] |
[
1,
0,
0,
0
] |
Which of the following best describe a spherical aberration?
A. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
B. dispersion of the light due to the refractive index of a lens being a function of the wavelength
C. when a sharp image is formed on a focal surface which isn't flat
D. when an otherwise sharp image is distorted in shape, such as when straight light on the surface being viewed appear curved on the focal plane
|
A. when light from the periphery of a spherical lens or mirror is focused nearer the element than light from the center
|
177
|
6a6dcec7-6109-4832-8981-f221e2f9e28e
|
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
| 0
|
[
"DR = Ne / Nr = 1460",
"DR = sqrt(Ne) / Nr = 0.54",
"DR = Neˆ2 / Nr = 1.07e10"
] |
[
1,
0,
0
] |
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
A. DR = Ne / Nr = 1460
B. DR = sqrt(Ne) / Nr = 0.54
C. DR = Neˆ2 / Nr = 1.07e10
|
A. DR = Ne / Nr = 1460
|
177
|
6a6dcec7-6109-4832-8981-f221e2f9e28e
|
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
| 1
|
[
"DR = sqrt(Ne) / Nr = 0.54",
"DR = Neˆ2 / Nr = 1.07e10",
"DR = Ne / Nr = 1460"
] |
[
0,
0,
1
] |
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
A. DR = sqrt(Ne) / Nr = 0.54
B. DR = Neˆ2 / Nr = 1.07e10
C. DR = Ne / Nr = 1460
|
C. DR = Ne / Nr = 1460
|
177
|
6a6dcec7-6109-4832-8981-f221e2f9e28e
|
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
| 2
|
[
"DR = Neˆ2 / Nr = 1.07e10",
"DR = Ne / Nr = 1460",
"DR = sqrt(Ne) / Nr = 0.54"
] |
[
0,
1,
0
] |
Assuming you are calculating parameters for a passive optical sensor, what would be the sensor dynamic range DR (with respect to cold space) assuming that the number of photocarriers available Ne = 7.3e6 (evaluated for an ideal detector) and number of read-out noise electrons is Nr = 5000?
A. DR = Neˆ2 / Nr = 1.07e10
B. DR = Ne / Nr = 1460
C. DR = sqrt(Ne) / Nr = 0.54
|
B. DR = Ne / Nr = 1460
|
178
|
b5555ff7-242f-4fe4-8734-7148627758e7
|
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
| 0
|
[
"Magnetometer",
"Star Sensor",
"Sun Sensor"
] |
[
0,
0,
1
] |
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
A. Magnetometer
B. Star Sensor
C. Sun Sensor
|
C. Sun Sensor
|
178
|
b5555ff7-242f-4fe4-8734-7148627758e7
|
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
| 1
|
[
"Star Sensor",
"Sun Sensor",
"Magnetometer"
] |
[
0,
1,
0
] |
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
A. Star Sensor
B. Sun Sensor
C. Magnetometer
|
B. Sun Sensor
|
178
|
b5555ff7-242f-4fe4-8734-7148627758e7
|
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
| 2
|
[
"Star Sensor",
"Magnetometer",
"Sun Sensor"
] |
[
0,
0,
1
] |
Which type of satellite sensor should you select for you AOCS if you need an accuracy of 0.1 deg and have string mass constraint?
A. Star Sensor
B. Magnetometer
C. Sun Sensor
|
C. Sun Sensor
|
179
|
34f1d6d5-a95f-4e56-b19c-8a54a8cb5da3
|
Which of the following definition is correct in the domain of spacecraft mechanisms?
| 0
|
[
"Deployables - devices used to provide optical adjustments for space instruments",
"Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical",
"Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing"
] |
[
0,
1,
0
] |
Which of the following definition is correct in the domain of spacecraft mechanisms?
A. Deployables - devices used to provide optical adjustments for space instruments
B. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
C. Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing
|
B. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
|
179
|
34f1d6d5-a95f-4e56-b19c-8a54a8cb5da3
|
Which of the following definition is correct in the domain of spacecraft mechanisms?
| 1
|
[
"Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical",
"Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing",
"Deployables - devices used to provide optical adjustments for space instruments"
] |
[
1,
0,
0
] |
Which of the following definition is correct in the domain of spacecraft mechanisms?
A. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
B. Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing
C. Deployables - devices used to provide optical adjustments for space instruments
|
A. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
|
179
|
34f1d6d5-a95f-4e56-b19c-8a54a8cb5da3
|
Which of the following definition is correct in the domain of spacecraft mechanisms?
| 2
|
[
"Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical",
"Deployables - devices used to provide optical adjustments for space instruments",
"Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing"
] |
[
1,
0,
0
] |
Which of the following definition is correct in the domain of spacecraft mechanisms?
A. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
B. Deployables - devices used to provide optical adjustments for space instruments
C. Instrument mechanisms - devices generally used to create spacecraft on-orbit configurations which are larger than can be packed in the launch vehicle fairing
|
A. Drives - devices requiring continuous or frequent operation for the life of the mission where wear, lubrication and life are critical
|
180
|
8c856182-3296-4088-b56f-9be8c16eb27e
|
What is true about MLI for satellites?
| 0
|
[
"MLI stands for Micro Layer Insulation",
"MLI stands for Multiple Layer Insulation",
"Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh",
"Composed of multiples layers of low-emittance films with low conductivity"
] |
[
0,
1,
0,
1
] |
What is true about MLI for satellites?
A. MLI stands for Micro Layer Insulation
B. MLI stands for Multiple Layer Insulation
C. Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh
D. Composed of multiples layers of low-emittance films with low conductivity
|
B. MLI stands for Multiple Layer Insulation
D. Composed of multiples layers of low-emittance films with low conductivity
|
180
|
8c856182-3296-4088-b56f-9be8c16eb27e
|
What is true about MLI for satellites?
| 1
|
[
"Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh",
"MLI stands for Micro Layer Insulation",
"MLI stands for Multiple Layer Insulation",
"Composed of multiples layers of low-emittance films with low conductivity"
] |
[
0,
0,
1,
1
] |
What is true about MLI for satellites?
A. Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh
B. MLI stands for Micro Layer Insulation
C. MLI stands for Multiple Layer Insulation
D. Composed of multiples layers of low-emittance films with low conductivity
|
C. MLI stands for Multiple Layer Insulation
D. Composed of multiples layers of low-emittance films with low conductivity
|
180
|
8c856182-3296-4088-b56f-9be8c16eb27e
|
What is true about MLI for satellites?
| 2
|
[
"MLI stands for Multiple Layer Insulation",
"Composed of multiples layers of low-emittance films with low conductivity",
"MLI stands for Micro Layer Insulation",
"Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh"
] |
[
1,
1,
0,
0
] |
What is true about MLI for satellites?
A. MLI stands for Multiple Layer Insulation
B. Composed of multiples layers of low-emittance films with low conductivity
C. MLI stands for Micro Layer Insulation
D. Composed of micrometer thickness layers of high-emittance films sandwiched with carbon fiber reinforced mesh
|
A. MLI stands for Multiple Layer Insulation
B. Composed of multiples layers of low-emittance films with low conductivity
|
181
|
a63a44bc-930e-4048-986e-2a2f80bf4a53
|
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
| 0
|
[
"Convection",
"Conduction",
"Radiation"
] |
[
1,
0,
0
] |
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
A. Convection
B. Conduction
C. Radiation
|
A. Convection
|
181
|
a63a44bc-930e-4048-986e-2a2f80bf4a53
|
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
| 1
|
[
"Radiation",
"Conduction",
"Convection"
] |
[
0,
0,
1
] |
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
A. Radiation
B. Conduction
C. Convection
|
C. Convection
|
181
|
a63a44bc-930e-4048-986e-2a2f80bf4a53
|
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
| 2
|
[
"Convection",
"Radiation",
"Conduction"
] |
[
1,
0,
0
] |
Which of the following thermal dissipation mechanism is usually not accounted for for satellite thermal balance?
A. Convection
B. Radiation
C. Conduction
|
A. Convection
|
182
|
d03a4ef0-162b-470d-969e-b7a2b75d223b
|
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
| 0
|
[
"Patch heater",
"Surface finish",
"Grooved Heat pipe",
"Cartridge heater",
"Louvers"
] |
[
0,
0,
0,
1,
0
] |
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
A. Patch heater
B. Surface finish
C. Grooved Heat pipe
D. Cartridge heater
E. Louvers
|
D. Cartridge heater
|
182
|
d03a4ef0-162b-470d-969e-b7a2b75d223b
|
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
| 1
|
[
"Cartridge heater",
"Grooved Heat pipe",
"Louvers",
"Patch heater",
"Surface finish"
] |
[
1,
0,
0,
0,
0
] |
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
A. Cartridge heater
B. Grooved Heat pipe
C. Louvers
D. Patch heater
E. Surface finish
|
A. Cartridge heater
|
182
|
d03a4ef0-162b-470d-969e-b7a2b75d223b
|
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
| 2
|
[
"Surface finish",
"Patch heater",
"Louvers",
"Cartridge heater",
"Grooved Heat pipe"
] |
[
0,
0,
0,
1,
0
] |
Which of the following thermal control component is used to warmup the catalyst bed of hydrazine thrusters?
A. Surface finish
B. Patch heater
C. Louvers
D. Cartridge heater
E. Grooved Heat pipe
|
D. Cartridge heater
|
183
|
af4a6b5c-618a-4ce9-bbeb-f3c3d6252467
|
Which of the following reviews according to European Space Agency space program life cycle comes last?
| 0
|
[
"PDR",
"SRR",
"MCR",
"CDR"
] |
[
0,
0,
0,
1
] |
Which of the following reviews according to European Space Agency space program life cycle comes last?
A. PDR
B. SRR
C. MCR
D. CDR
|
D. CDR
|
183
|
af4a6b5c-618a-4ce9-bbeb-f3c3d6252467
|
Which of the following reviews according to European Space Agency space program life cycle comes last?
| 1
|
[
"SRR",
"MCR",
"CDR",
"PDR"
] |
[
0,
0,
1,
0
] |
Which of the following reviews according to European Space Agency space program life cycle comes last?
A. SRR
B. MCR
C. CDR
D. PDR
|
C. CDR
|
183
|
af4a6b5c-618a-4ce9-bbeb-f3c3d6252467
|
Which of the following reviews according to European Space Agency space program life cycle comes last?
| 2
|
[
"CDR",
"PDR",
"MCR",
"SRR"
] |
[
1,
0,
0,
0
] |
Which of the following reviews according to European Space Agency space program life cycle comes last?
A. CDR
B. PDR
C. MCR
D. SRR
|
A. CDR
|
184
|
ebd7de2e-9dea-4aad-be29-3587856b4e75
|
Select all which are commonly accepted end item verification methods?
| 0
|
[
"Verification by similarity",
"Verification by test",
"Verification by analysis",
"Verification by inspection"
] |
[
1,
1,
1,
1
] |
Select all which are commonly accepted end item verification methods?
A. Verification by similarity
B. Verification by test
C. Verification by analysis
D. Verification by inspection
|
A. Verification by similarity
B. Verification by test
C. Verification by analysis
D. Verification by inspection
|
184
|
ebd7de2e-9dea-4aad-be29-3587856b4e75
|
Select all which are commonly accepted end item verification methods?
| 1
|
[
"Verification by analysis",
"Verification by test",
"Verification by inspection",
"Verification by similarity"
] |
[
1,
1,
1,
1
] |
Select all which are commonly accepted end item verification methods?
A. Verification by analysis
B. Verification by test
C. Verification by inspection
D. Verification by similarity
|
A. Verification by analysis
B. Verification by test
C. Verification by inspection
D. Verification by similarity
|
184
|
ebd7de2e-9dea-4aad-be29-3587856b4e75
|
Select all which are commonly accepted end item verification methods?
| 2
|
[
"Verification by analysis",
"Verification by similarity",
"Verification by test",
"Verification by inspection"
] |
[
1,
1,
1,
1
] |
Select all which are commonly accepted end item verification methods?
A. Verification by analysis
B. Verification by similarity
C. Verification by test
D. Verification by inspection
|
A. Verification by analysis
B. Verification by similarity
C. Verification by test
D. Verification by inspection
|
185
|
828838d1-992e-412b-91ea-fe10ed216ec5
|
What are burn-in tests for spacecraft components?
| 0
|
[
"application of electrical stresses above normal use, or rating, usually high voltage",
"application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)",
"application of radiation stesses simulating single events",
"application of pseudo-random vibration spectum predicted for launch and atmospheric ascent",
"sustained high temperature operation over pre-defined time span"
] |
[
0,
0,
0,
0,
1
] |
What are burn-in tests for spacecraft components?
A. application of electrical stresses above normal use, or rating, usually high voltage
B. application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)
C. application of radiation stesses simulating single events
D. application of pseudo-random vibration spectum predicted for launch and atmospheric ascent
E. sustained high temperature operation over pre-defined time span
|
E. sustained high temperature operation over pre-defined time span
|
185
|
828838d1-992e-412b-91ea-fe10ed216ec5
|
What are burn-in tests for spacecraft components?
| 1
|
[
"application of radiation stesses simulating single events",
"sustained high temperature operation over pre-defined time span",
"application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)",
"application of pseudo-random vibration spectum predicted for launch and atmospheric ascent",
"application of electrical stresses above normal use, or rating, usually high voltage"
] |
[
0,
1,
0,
0,
0
] |
What are burn-in tests for spacecraft components?
A. application of radiation stesses simulating single events
B. sustained high temperature operation over pre-defined time span
C. application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)
D. application of pseudo-random vibration spectum predicted for launch and atmospheric ascent
E. application of electrical stresses above normal use, or rating, usually high voltage
|
B. sustained high temperature operation over pre-defined time span
|
185
|
828838d1-992e-412b-91ea-fe10ed216ec5
|
What are burn-in tests for spacecraft components?
| 2
|
[
"application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)",
"application of pseudo-random vibration spectum predicted for launch and atmospheric ascent",
"application of electrical stresses above normal use, or rating, usually high voltage",
"sustained high temperature operation over pre-defined time span",
"application of radiation stesses simulating single events"
] |
[
0,
0,
0,
1,
0
] |
What are burn-in tests for spacecraft components?
A. application of transients simulating those resulting from sudden release of loads (staging/separation, deployment)
B. application of pseudo-random vibration spectum predicted for launch and atmospheric ascent
C. application of electrical stresses above normal use, or rating, usually high voltage
D. sustained high temperature operation over pre-defined time span
E. application of radiation stesses simulating single events
|
D. sustained high temperature operation over pre-defined time span
|
186
|
2147b0f6-662f-4872-8b8e-18e280d5e29d
|
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
| 0
|
[
"Thermal vacuum",
"Pyro-shock",
"Burn-in",
"Thermal cycling",
"Enhanced low dose rate sensitivity (ELDRS)"
] |
[
0,
0,
0,
1,
0
] |
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
A. Thermal vacuum
B. Pyro-shock
C. Burn-in
D. Thermal cycling
E. Enhanced low dose rate sensitivity (ELDRS)
|
D. Thermal cycling
|
186
|
2147b0f6-662f-4872-8b8e-18e280d5e29d
|
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
| 1
|
[
"Thermal cycling",
"Burn-in",
"Thermal vacuum",
"Enhanced low dose rate sensitivity (ELDRS)",
"Pyro-shock"
] |
[
1,
0,
0,
0,
0
] |
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
A. Thermal cycling
B. Burn-in
C. Thermal vacuum
D. Enhanced low dose rate sensitivity (ELDRS)
E. Pyro-shock
|
A. Thermal cycling
|
186
|
2147b0f6-662f-4872-8b8e-18e280d5e29d
|
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
| 2
|
[
"Thermal cycling",
"Burn-in",
"Thermal vacuum",
"Pyro-shock",
"Enhanced low dose rate sensitivity (ELDRS)"
] |
[
1,
0,
0,
0,
0
] |
What type of environmental tests for units under tests correspond to rapid temperature transitions between defined extremes under normal atmospheric conditions, dwelling at extremes for hours at a time?
A. Thermal cycling
B. Burn-in
C. Thermal vacuum
D. Pyro-shock
E. Enhanced low dose rate sensitivity (ELDRS)
|
A. Thermal cycling
|
187
|
beb8a417-4d86-44f1-b07b-e3ba7dbf6194
|
How can you compute the MTBF assuming you know the failure rate lambda?
| 0
|
[
"lambda / (1 - lambda)",
"lambdaˆ2",
"lambdaˆ(1/2)",
"1 / lambda"
] |
[
0,
0,
0,
1
] |
How can you compute the MTBF assuming you know the failure rate lambda?
A. lambda / (1 - lambda)
B. lambdaˆ2
C. lambdaˆ(1/2)
D. 1 / lambda
|
D. 1 / lambda
|
187
|
beb8a417-4d86-44f1-b07b-e3ba7dbf6194
|
How can you compute the MTBF assuming you know the failure rate lambda?
| 1
|
[
"lambdaˆ(1/2)",
"1 / lambda",
"lambdaˆ2",
"lambda / (1 - lambda)"
] |
[
0,
1,
0,
0
] |
How can you compute the MTBF assuming you know the failure rate lambda?
A. lambdaˆ(1/2)
B. 1 / lambda
C. lambdaˆ2
D. lambda / (1 - lambda)
|
B. 1 / lambda
|
187
|
beb8a417-4d86-44f1-b07b-e3ba7dbf6194
|
How can you compute the MTBF assuming you know the failure rate lambda?
| 2
|
[
"1 / lambda",
"lambda / (1 - lambda)",
"lambdaˆ2",
"lambdaˆ(1/2)"
] |
[
1,
0,
0,
0
] |
How can you compute the MTBF assuming you know the failure rate lambda?
A. 1 / lambda
B. lambda / (1 - lambda)
C. lambdaˆ2
D. lambdaˆ(1/2)
|
A. 1 / lambda
|
188
|
0908d052-016a-410e-a96c-ab10b813b4f6
|
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
| 0
|
[
"Approximately 0.02",
"Exactly 0.87",
"Approximately 0.03",
"Approximately 0.95",
"Approximately 0.97",
"Exactly 0.76"
] |
[
0,
0,
0,
0,
1,
0
] |
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
A. Approximately 0.02
B. Exactly 0.87
C. Approximately 0.03
D. Approximately 0.95
E. Approximately 0.97
F. Exactly 0.76
|
E. Approximately 0.97
|
188
|
0908d052-016a-410e-a96c-ab10b813b4f6
|
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
| 1
|
[
"Exactly 0.87",
"Approximately 0.03",
"Exactly 0.76",
"Approximately 0.02",
"Approximately 0.95",
"Approximately 0.97"
] |
[
0,
0,
0,
0,
0,
1
] |
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
A. Exactly 0.87
B. Approximately 0.03
C. Exactly 0.76
D. Approximately 0.02
E. Approximately 0.95
F. Approximately 0.97
|
F. Approximately 0.97
|
188
|
0908d052-016a-410e-a96c-ab10b813b4f6
|
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
| 2
|
[
"Approximately 0.95",
"Exactly 0.76",
"Approximately 0.03",
"Approximately 0.97",
"Approximately 0.02",
"Exactly 0.87"
] |
[
0,
0,
0,
1,
0,
0
] |
Consider a propellant feed system with two valves in series. Valve one has a probability of failure in close position of 0.01 and the other valve has a probability of failure in close position of 0.02. If any of the valve fail in the close position, the propellant cannot flow anymore. What is the overall reliability R of the feed system to still be open?
A. Approximately 0.95
B. Exactly 0.76
C. Approximately 0.03
D. Approximately 0.97
E. Approximately 0.02
F. Exactly 0.87
|
D. Approximately 0.97
|
189
|
1f9fc6c5-c327-4450-80bf-270c646f093d
|
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
| 0
|
[
"English",
"Russian",
"French",
"Japanese",
"Chinese"
] |
[
1,
1,
0,
0,
0
] |
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
A. English
B. Russian
C. French
D. Japanese
E. Chinese
|
A. English
B. Russian
|
189
|
1f9fc6c5-c327-4450-80bf-270c646f093d
|
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
| 1
|
[
"Japanese",
"English",
"Russian",
"Chinese",
"French"
] |
[
0,
1,
1,
0,
0
] |
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
A. Japanese
B. English
C. Russian
D. Chinese
E. French
|
B. English
C. Russian
|
189
|
1f9fc6c5-c327-4450-80bf-270c646f093d
|
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
| 2
|
[
"Chinese",
"French",
"Russian",
"Japanese",
"English"
] |
[
0,
0,
1,
0,
1
] |
Which of the following languages will you have to learn as a minimum if your are selected as an Astronaut?
A. Chinese
B. French
C. Russian
D. Japanese
E. English
|
C. Russian
E. English
|
190
|
fba43aad-6a08-4d7a-946e-d73a65a99742
|
Which of this center are knwon for Astronaut training?
| 0
|
[
"Jet Propulsion Laboratory",
"Kennedy Space Center",
"ESA/ESTEC",
"ESA/EAC",
"Johnson Space Center",
"Star City"
] |
[
0,
0,
0,
1,
1,
1
] |
Which of this center are knwon for Astronaut training?
A. Jet Propulsion Laboratory
B. Kennedy Space Center
C. ESA/ESTEC
D. ESA/EAC
E. Johnson Space Center
F. Star City
|
D. ESA/EAC
E. Johnson Space Center
F. Star City
|
190
|
fba43aad-6a08-4d7a-946e-d73a65a99742
|
Which of this center are knwon for Astronaut training?
| 1
|
[
"ESA/EAC",
"Johnson Space Center",
"ESA/ESTEC",
"Star City",
"Jet Propulsion Laboratory",
"Kennedy Space Center"
] |
[
1,
1,
0,
1,
0,
0
] |
Which of this center are knwon for Astronaut training?
A. ESA/EAC
B. Johnson Space Center
C. ESA/ESTEC
D. Star City
E. Jet Propulsion Laboratory
F. Kennedy Space Center
|
A. ESA/EAC
B. Johnson Space Center
D. Star City
|
190
|
fba43aad-6a08-4d7a-946e-d73a65a99742
|
Which of this center are knwon for Astronaut training?
| 2
|
[
"ESA/EAC",
"Jet Propulsion Laboratory",
"Star City",
"ESA/ESTEC",
"Johnson Space Center",
"Kennedy Space Center"
] |
[
1,
0,
1,
0,
1,
0
] |
Which of this center are knwon for Astronaut training?
A. ESA/EAC
B. Jet Propulsion Laboratory
C. Star City
D. ESA/ESTEC
E. Johnson Space Center
F. Kennedy Space Center
|
A. ESA/EAC
C. Star City
E. Johnson Space Center
|
191
|
cf12aa3a-38cc-4067-b829-0510a550874e
|
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
| 0
|
[
"Centrifuges",
"Drop tower",
"zero-G flight",
"Water Buoyancy Lab"
] |
[
0,
0,
1,
0
] |
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
A. Centrifuges
B. Drop tower
C. zero-G flight
D. Water Buoyancy Lab
|
C. zero-G flight
|
191
|
cf12aa3a-38cc-4067-b829-0510a550874e
|
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
| 1
|
[
"Drop tower",
"Centrifuges",
"zero-G flight",
"Water Buoyancy Lab"
] |
[
0,
0,
1,
0
] |
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
A. Drop tower
B. Centrifuges
C. zero-G flight
D. Water Buoyancy Lab
|
C. zero-G flight
|
191
|
cf12aa3a-38cc-4067-b829-0510a550874e
|
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
| 2
|
[
"zero-G flight",
"Water Buoyancy Lab",
"Drop tower",
"Centrifuges"
] |
[
1,
0,
0,
0
] |
Which of the following system enable astronaut to experience up to 20 seconds of weightlessness?
A. zero-G flight
B. Water Buoyancy Lab
C. Drop tower
D. Centrifuges
|
A. zero-G flight
|
192
|
793b77a7-204e-4acc-a252-b56ed5e25263
|
What should you do first when a non-confirmance is detected according to the ECSS?
| 0
|
[
"Notify the customer and call out for a customer non-conformance review board (NRB)",
"Issue a non-conformance test plan (NCTP)",
"Implement corrective and preventive actions",
"Organize an internal non-conformance review board (NRB)",
"Call the supplier and fire them",
"Issue an internal Non-conformance report (NCR)"
] |
[
0,
0,
0,
0,
0,
1
] |
What should you do first when a non-confirmance is detected according to the ECSS?
A. Notify the customer and call out for a customer non-conformance review board (NRB)
B. Issue a non-conformance test plan (NCTP)
C. Implement corrective and preventive actions
D. Organize an internal non-conformance review board (NRB)
E. Call the supplier and fire them
F. Issue an internal Non-conformance report (NCR)
|
F. Issue an internal Non-conformance report (NCR)
|
192
|
793b77a7-204e-4acc-a252-b56ed5e25263
|
What should you do first when a non-confirmance is detected according to the ECSS?
| 1
|
[
"Issue an internal Non-conformance report (NCR)",
"Call the supplier and fire them",
"Issue a non-conformance test plan (NCTP)",
"Organize an internal non-conformance review board (NRB)",
"Implement corrective and preventive actions",
"Notify the customer and call out for a customer non-conformance review board (NRB)"
] |
[
1,
0,
0,
0,
0,
0
] |
What should you do first when a non-confirmance is detected according to the ECSS?
A. Issue an internal Non-conformance report (NCR)
B. Call the supplier and fire them
C. Issue a non-conformance test plan (NCTP)
D. Organize an internal non-conformance review board (NRB)
E. Implement corrective and preventive actions
F. Notify the customer and call out for a customer non-conformance review board (NRB)
|
A. Issue an internal Non-conformance report (NCR)
|
192
|
793b77a7-204e-4acc-a252-b56ed5e25263
|
What should you do first when a non-confirmance is detected according to the ECSS?
| 2
|
[
"Organize an internal non-conformance review board (NRB)",
"Notify the customer and call out for a customer non-conformance review board (NRB)",
"Issue an internal Non-conformance report (NCR)",
"Issue a non-conformance test plan (NCTP)",
"Implement corrective and preventive actions",
"Call the supplier and fire them"
] |
[
0,
0,
1,
0,
0,
0
] |
What should you do first when a non-confirmance is detected according to the ECSS?
A. Organize an internal non-conformance review board (NRB)
B. Notify the customer and call out for a customer non-conformance review board (NRB)
C. Issue an internal Non-conformance report (NCR)
D. Issue a non-conformance test plan (NCTP)
E. Implement corrective and preventive actions
F. Call the supplier and fire them
|
C. Issue an internal Non-conformance report (NCR)
|
193
|
7e74f9c0-2899-40b3-a143-19cd380ebdd2
|
Which of the following are commonly accepted dispositions of minor non-conformances?
| 0
|
[
"Repair",
"Test again until test pass",
"Rework",
"Scrap",
"Return to supplier",
"Use \"As Is\""
] |
[
1,
0,
1,
1,
1,
1
] |
Which of the following are commonly accepted dispositions of minor non-conformances?
A. Repair
B. Test again until test pass
C. Rework
D. Scrap
E. Return to supplier
F. Use "As Is"
|
A. Repair
C. Rework
D. Scrap
E. Return to supplier
F. Use "As Is"
|
193
|
7e74f9c0-2899-40b3-a143-19cd380ebdd2
|
Which of the following are commonly accepted dispositions of minor non-conformances?
| 1
|
[
"Return to supplier",
"Scrap",
"Rework",
"Use \"As Is\"",
"Repair",
"Test again until test pass"
] |
[
1,
1,
1,
1,
1,
0
] |
Which of the following are commonly accepted dispositions of minor non-conformances?
A. Return to supplier
B. Scrap
C. Rework
D. Use "As Is"
E. Repair
F. Test again until test pass
|
A. Return to supplier
B. Scrap
C. Rework
D. Use "As Is"
E. Repair
|
193
|
7e74f9c0-2899-40b3-a143-19cd380ebdd2
|
Which of the following are commonly accepted dispositions of minor non-conformances?
| 2
|
[
"Repair",
"Scrap",
"Rework",
"Test again until test pass",
"Return to supplier",
"Use \"As Is\""
] |
[
1,
1,
1,
0,
1,
1
] |
Which of the following are commonly accepted dispositions of minor non-conformances?
A. Repair
B. Scrap
C. Rework
D. Test again until test pass
E. Return to supplier
F. Use "As Is"
|
A. Repair
B. Scrap
C. Rework
E. Return to supplier
F. Use "As Is"
|
194
|
6e49ffae-e12f-4053-b482-0f35294b805c
|
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
| 0
|
[
"Geostationary Orbit",
"Sun Synchronous Orbit",
"Korolev Orbit",
"Molniya Orbit",
"Kennedy Orbit",
"Polar Orbit"
] |
[
0,
0,
0,
1,
0,
0
] |
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
A. Geostationary Orbit
B. Sun Synchronous Orbit
C. Korolev Orbit
D. Molniya Orbit
E. Kennedy Orbit
F. Polar Orbit
|
D. Molniya Orbit
|
194
|
6e49ffae-e12f-4053-b482-0f35294b805c
|
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
| 1
|
[
"Molniya Orbit",
"Geostationary Orbit",
"Sun Synchronous Orbit",
"Korolev Orbit",
"Kennedy Orbit",
"Polar Orbit"
] |
[
1,
0,
0,
0,
0,
0
] |
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
A. Molniya Orbit
B. Geostationary Orbit
C. Sun Synchronous Orbit
D. Korolev Orbit
E. Kennedy Orbit
F. Polar Orbit
|
A. Molniya Orbit
|
194
|
6e49ffae-e12f-4053-b482-0f35294b805c
|
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
| 2
|
[
"Sun Synchronous Orbit",
"Korolev Orbit",
"Polar Orbit",
"Molniya Orbit",
"Geostationary Orbit",
"Kennedy Orbit"
] |
[
0,
0,
0,
1,
0,
0
] |
What type of orbit is famous for its long dwell time over North America and Russia while passeing quickly over the southern hemisphere?
A. Sun Synchronous Orbit
B. Korolev Orbit
C. Polar Orbit
D. Molniya Orbit
E. Geostationary Orbit
F. Kennedy Orbit
|
D. Molniya Orbit
|
195
|
80f3bfa3-5198-4c0f-a137-4c679b192a58
|
Which of the following gas is the main component of the Mars atmosphere?
| 0
|
[
"CO2",
"O2",
"CH4",
"Ar",
"N2"
] |
[
1,
0,
0,
0,
0
] |
Which of the following gas is the main component of the Mars atmosphere?
A. CO2
B. O2
C. CH4
D. Ar
E. N2
|
A. CO2
|
195
|
80f3bfa3-5198-4c0f-a137-4c679b192a58
|
Which of the following gas is the main component of the Mars atmosphere?
| 1
|
[
"O2",
"N2",
"Ar",
"CO2",
"CH4"
] |
[
0,
0,
0,
1,
0
] |
Which of the following gas is the main component of the Mars atmosphere?
A. O2
B. N2
C. Ar
D. CO2
E. CH4
|
D. CO2
|
195
|
80f3bfa3-5198-4c0f-a137-4c679b192a58
|
Which of the following gas is the main component of the Mars atmosphere?
| 2
|
[
"N2",
"Ar",
"CH4",
"O2",
"CO2"
] |
[
0,
0,
0,
0,
1
] |
Which of the following gas is the main component of the Mars atmosphere?
A. N2
B. Ar
C. CH4
D. O2
E. CO2
|
E. CO2
|
196
|
73f86516-6e00-4668-91e8-9e15ebb3912e
|
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
| 0
|
[
"3500 hours",
"35 hours",
"350 hours",
"3.5 hours"
] |
[
0,
0,
1,
0
] |
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
A. 3500 hours
B. 35 hours
C. 350 hours
D. 3.5 hours
|
C. 350 hours
|
196
|
73f86516-6e00-4668-91e8-9e15ebb3912e
|
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
| 1
|
[
"350 hours",
"35 hours",
"3.5 hours",
"3500 hours"
] |
[
1,
0,
0,
0
] |
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
A. 350 hours
B. 35 hours
C. 3.5 hours
D. 3500 hours
|
A. 350 hours
|
196
|
73f86516-6e00-4668-91e8-9e15ebb3912e
|
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
| 2
|
[
"3500 hours",
"350 hours",
"3.5 hours",
"35 hours"
] |
[
0,
1,
0,
0
] |
How long do Lunar night last near the Moon equator (period of time where your solar array will not generate electricity and where you would have to run on batteries)
A. 3500 hours
B. 350 hours
C. 3.5 hours
D. 35 hours
|
B. 350 hours
|
197
|
10a3f4eb-6269-41c8-9a78-410ff0189ffb
|
Which can you find on the Moon surface?
| 0
|
[
"Ilmenite",
"A thin atmosphere",
"Lava tubes",
"Iron, Titanium, and Aluminum oxides",
"Liquid methane"
] |
[
1,
0,
1,
1,
0
] |
Which can you find on the Moon surface?
A. Ilmenite
B. A thin atmosphere
C. Lava tubes
D. Iron, Titanium, and Aluminum oxides
E. Liquid methane
|
A. Ilmenite
C. Lava tubes
D. Iron, Titanium, and Aluminum oxides
|
197
|
10a3f4eb-6269-41c8-9a78-410ff0189ffb
|
Which can you find on the Moon surface?
| 1
|
[
"Lava tubes",
"Ilmenite",
"Liquid methane",
"Iron, Titanium, and Aluminum oxides",
"A thin atmosphere"
] |
[
1,
1,
0,
1,
0
] |
Which can you find on the Moon surface?
A. Lava tubes
B. Ilmenite
C. Liquid methane
D. Iron, Titanium, and Aluminum oxides
E. A thin atmosphere
|
A. Lava tubes
B. Ilmenite
D. Iron, Titanium, and Aluminum oxides
|
197
|
10a3f4eb-6269-41c8-9a78-410ff0189ffb
|
Which can you find on the Moon surface?
| 2
|
[
"Iron, Titanium, and Aluminum oxides",
"Ilmenite",
"Liquid methane",
"A thin atmosphere",
"Lava tubes"
] |
[
1,
1,
0,
0,
1
] |
Which can you find on the Moon surface?
A. Iron, Titanium, and Aluminum oxides
B. Ilmenite
C. Liquid methane
D. A thin atmosphere
E. Lava tubes
|
A. Iron, Titanium, and Aluminum oxides
B. Ilmenite
E. Lava tubes
|
198
|
ed958ac6-616f-479d-b73c-203016fdf5d5
|
Which mission types to Mars often include a Venus fly-by?
| 0
|
[
"J-type mission",
"Opposition mission",
"S-type mission",
"Cross-trapped mission",
"Conjunction mission"
] |
[
0,
1,
0,
0,
0
] |
Which mission types to Mars often include a Venus fly-by?
A. J-type mission
B. Opposition mission
C. S-type mission
D. Cross-trapped mission
E. Conjunction mission
|
B. Opposition mission
|
198
|
ed958ac6-616f-479d-b73c-203016fdf5d5
|
Which mission types to Mars often include a Venus fly-by?
| 1
|
[
"S-type mission",
"Cross-trapped mission",
"Opposition mission",
"Conjunction mission",
"J-type mission"
] |
[
0,
0,
1,
0,
0
] |
Which mission types to Mars often include a Venus fly-by?
A. S-type mission
B. Cross-trapped mission
C. Opposition mission
D. Conjunction mission
E. J-type mission
|
C. Opposition mission
|
198
|
ed958ac6-616f-479d-b73c-203016fdf5d5
|
Which mission types to Mars often include a Venus fly-by?
| 2
|
[
"Opposition mission",
"Conjunction mission",
"Cross-trapped mission",
"J-type mission",
"S-type mission"
] |
[
1,
0,
0,
0,
0
] |
Which mission types to Mars often include a Venus fly-by?
A. Opposition mission
B. Conjunction mission
C. Cross-trapped mission
D. J-type mission
E. S-type mission
|
A. Opposition mission
|
199
|
1e79fa37-6af1-4a77-9b9d-5f448a7924e4
|
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
| 0
|
[
"Book-keeping",
"Pressure-Volume-Temperature",
"Station-keeping",
"Entropy-Enthalpy-Gibbs"
] |
[
1,
1,
0,
0
] |
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
A. Book-keeping
B. Pressure-Volume-Temperature
C. Station-keeping
D. Entropy-Enthalpy-Gibbs
|
A. Book-keeping
B. Pressure-Volume-Temperature
|
199
|
1e79fa37-6af1-4a77-9b9d-5f448a7924e4
|
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
| 1
|
[
"Station-keeping",
"Entropy-Enthalpy-Gibbs",
"Pressure-Volume-Temperature",
"Book-keeping"
] |
[
0,
0,
1,
1
] |
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
A. Station-keeping
B. Entropy-Enthalpy-Gibbs
C. Pressure-Volume-Temperature
D. Book-keeping
|
C. Pressure-Volume-Temperature
D. Book-keeping
|
199
|
1e79fa37-6af1-4a77-9b9d-5f448a7924e4
|
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
| 2
|
[
"Pressure-Volume-Temperature",
"Book-keeping",
"Entropy-Enthalpy-Gibbs",
"Station-keeping"
] |
[
1,
1,
0,
0
] |
Which of the following methods are well known for propellant gauging in satellite propellant subsystems?
A. Pressure-Volume-Temperature
B. Book-keeping
C. Entropy-Enthalpy-Gibbs
D. Station-keeping
|
A. Pressure-Volume-Temperature
B. Book-keeping
|
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